| CPC B64C 25/405 (2013.01) | 19 Claims |

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1. A wheel acceleration system configured to apply a motive force to a wheel mounted to a landing gear of an aircraft, the wheel acceleration system comprising:
a pyrotechnic unit configured to generate expanding gases by combusting a propellant;
a rotary propulsion unit pneumatically coupled to the pyrotechnic unit, the rotary propulsion unit comprising an impeller configured to be driven by the expanding gases and to deliver torque to the wheel; and
an overdriving clutch coupling the impeller to the wheel.
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